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Influence of intensive suction on the flow in the neighborhood of a laminar-boundary-layer separation point in a supersonic flow

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Literature cited

  1. F. W. Meredith and A. A. Griffith, “Control with auxiliary power. Diffusera,” Modern Developments in Fluid Dynamics, Vol. 2, Oxford Univ. Press (1938).

  2. H. Schlichting, “Die Grenzschicht mit Absaugung und Ausblasen,” Luftfahrt-Forschung,19, No. 5 (1942).

  3. H. Schlichting, Boundary Layer Theory, McGraw-Hill (1968).

  4. H. G. Lew, “On the compressible boundary layer over a flat plate with uniform suction,” Reisner Annivers. Volume, J. W. Edwards (1949).

  5. A. D. Young, “Note on the velocity and temperature distributions attained with suctions on a flat plate of infinite extent in a compressible flow,” Quart. J. Mech. and Appl. Math.,1, No. 1 (1948).

  6. V. Ya. Neiland, “On the theory of laminar boundary-layer separation in a supersonic flow,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 4 (1969).

  7. V. Ya. Neiland, “Flow behind the boundary-layer separation point in a supersonic stream,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 3 (1971).

  8. V. Ya. Neiland, “On the asymptotic theory of supersonic-stream interaction with a boundary layer,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 4 (1971).

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Authors and Affiliations

  1. Moscow

    I. I. Lipatov & V. Ya. Neiland

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  1. I. I. Lipatov
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  2. V. Ya. Neiland
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 2, pp. 17–22, March–April, 1974.

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Lipatov, I.I., Neiland, V.Y. Influence of intensive suction on the flow in the neighborhood of a laminar-boundary-layer separation point in a supersonic flow. Fluid Dyn 9, 173–178 (1974). https://doi.org/10.1007/BF01092646

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  • DOI: https://doi.org/10.1007/BF01092646

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